Statements (53)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:Sir_Henry_Royce
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:compression_ratio |
5.5:1
|
| gptkbp:cooling_system |
liquid cooling
water-cooled |
| gptkbp:displacement |
12.0 L
|
| gptkbp:engine |
gptkb:V12
gptkb:12 high reliability high power-to-weight ratio V configuration inline engine detailed specifications available produced in large numbers introduced several engineering innovations influenced future engine designs focused on performance and reliability renowned for quality and performance early 20th century aircraft widely used in various aircraft models developed during World War I produced in the UK features advanced engineering for its time contributed to advancements in aviation engines contributed to the development of V12 engines. important in the context of aviation history notable for its smooth operation part of Rolls-Royce's early aviation history |
| gptkbp:engine_type |
gptkb:Rolls-Royce_110_HP
|
| gptkbp:first_introduced |
gptkb:1914
|
| gptkbp:fuel_capacity |
approximately 1.5 m
approximately 0.8 m approximately 0.6 m |
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce 100 HP
|
| gptkbp:ignition_system |
magneto ignition
|
| gptkbp:impact |
significant impact on aviation technology
|
| gptkbp:is_tested_for |
extensively tested
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notable_users |
gptkb:Royal_Flying_Corps
|
| gptkbp:power_output |
100 hp
|
| gptkbp:production_years |
1914-1918
|
| gptkbp:propulsion |
fixed-pitch propeller
|
| gptkbp:replaced_by |
gptkb:Rolls-Royce_Eagle_engine
|
| gptkbp:setting |
liquid-cooled
|
| gptkbp:successor |
gptkb:Rolls-Royce_Eagle
|
| gptkbp:torque |
wet sump
|
| gptkbp:type |
V-12 engine
|
| gptkbp:used_in |
gptkb:aircraft
|
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
approximately 200 lb
|